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    A Zonal Approach for Navier–Stokes Computations of Compressible Cascade Flow Fields Using a TVD Finite Volume Method

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 004::page 573
    Author:
    M. Furukawa
    ,
    M. Yamasaki
    ,
    M. Inoue
    DOI: 10.1115/1.2929118
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new zonal approach for computation of compressible viscous flows in cascades has been developed. The two-dimensional, Reynolds-averaged Navier–Stokes equations are discretized spatially by a cell-centered finite volume formulation. In order to make the present approach robust, the inviscid fluxes at cell interfaces are evaluated using a highly accurate TVD scheme based on the MUSCL-type approach with the Roe’s approximate Riemann solver. The viscous fluxes are determined in a central differencing manner. To simplify the grid generation, a composite zonal grid system is adopted, in which the computational domain is divided into nonoverlapping zones, and structured grids are generated independently in each zone. The zonal boundary between two zones is uniquely defined by cell interfaces of one zone, which ensures the uniqueness of the zonal boundary. Communication from one zone to the other is accomplished by numerical fluxes across the zonal boundary. It should be noted that the complete conservation of the numerical fluxes across the zonal boundary can be satisfied by directly evaluating the numerical fluxes using the finite volume method and by ensuring the uniqueness of the zonal boundary. In order to demonstrate the versatility of the present zonal approach, numerical examples are presented for viscous flows through a transonic turbine cascade.
    keyword(s): Flow (Dynamics) , Computation , Finite volume methods , Flux (Metallurgy) , Cascades (Fluid dynamics) , Turbines , Composite materials , Mesh generation AND Reynolds-averaged Navier–Stokes equations ,
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      A Zonal Approach for Navier–Stokes Computations of Compressible Cascade Flow Fields Using a TVD Finite Volume Method

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/109350
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    • Journal of Turbomachinery

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    contributor authorM. Furukawa
    contributor authorM. Yamasaki
    contributor authorM. Inoue
    date accessioned2017-05-08T23:36:53Z
    date available2017-05-08T23:36:53Z
    date copyrightOctober, 1991
    date issued1991
    identifier issn0889-504X
    identifier otherJOTUEI-28615#573_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109350
    description abstractA new zonal approach for computation of compressible viscous flows in cascades has been developed. The two-dimensional, Reynolds-averaged Navier–Stokes equations are discretized spatially by a cell-centered finite volume formulation. In order to make the present approach robust, the inviscid fluxes at cell interfaces are evaluated using a highly accurate TVD scheme based on the MUSCL-type approach with the Roe’s approximate Riemann solver. The viscous fluxes are determined in a central differencing manner. To simplify the grid generation, a composite zonal grid system is adopted, in which the computational domain is divided into nonoverlapping zones, and structured grids are generated independently in each zone. The zonal boundary between two zones is uniquely defined by cell interfaces of one zone, which ensures the uniqueness of the zonal boundary. Communication from one zone to the other is accomplished by numerical fluxes across the zonal boundary. It should be noted that the complete conservation of the numerical fluxes across the zonal boundary can be satisfied by directly evaluating the numerical fluxes using the finite volume method and by ensuring the uniqueness of the zonal boundary. In order to demonstrate the versatility of the present zonal approach, numerical examples are presented for viscous flows through a transonic turbine cascade.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Zonal Approach for Navier–Stokes Computations of Compressible Cascade Flow Fields Using a TVD Finite Volume Method
    typeJournal Paper
    journal volume113
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2929118
    journal fristpage573
    journal lastpage582
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsComputation
    keywordsFinite volume methods
    keywordsFlux (Metallurgy)
    keywordsCascades (Fluid dynamics)
    keywordsTurbines
    keywordsComposite materials
    keywordsMesh generation AND Reynolds-averaged Navier–Stokes equations
    treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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